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Updated: Jul 2, 2025

A Protocol for Real-time 3D Single Particle Tracking
Published on: January 3, 2018
空载星星追踪器的追踪方案基于事件触发的滑动模式控制,具有已知的输入延迟
Tianji Cheng1, Zhiwen Liu1, Shengjie Wei1
1National Key Laboratory of Optical Field Manipulation Science and Technology, Chengdu 610209, China; Institute of Optics and Electronics, Chinese Academy of Sciences, Chengdu 610209, China; Key Laboratory of Science and Technology on Space Optoelectronic Precision Measurement, Chinese Academy of Sciences, Chengdu 610209, China; University of Chinese Academy of Sciences, Beijing 100049, China.
这项研究引入了空中恒星追踪器的事件触发滑动模式控制 (ET-SMC),通过解决干扰和计算限制来提高导航准确性. 新型ET-SMC增强了稳定的飞机导航的稳定性和资源效率.
科学领域:
- 航空航天工程 航空航天工程
- 控制系统 控制系统
背景情况:
- 空载恒星追踪器对于飞机导航至关重要,但它们的性能受到环境干扰和有限的计算资源的影响.
- 现有的控制策略往往无法同时解决这些挑战.
研究的目的:
- 为空中恒星追踪器提出一个新的事件触发式滑动模式控制 (ET-SMC) 方案.
- 在已知输入时间延迟下解决恒星追踪控制中的干扰和计算限制.
主要方法:
- 一个扩展状态观察员 (ESO) 估计空中干扰.
- 一个基于ESO错误的事件触发机制的新型ET-SMC方案提高了稳定性和资源利用率.
- 一个新的滑动增益减少了喋喋不休,提高了适应性.
主要成果:
- 利亚普诺夫理论证实了系统稳定性,滑动表面的可达性和实际的滑动模式存在.
- 系统状态的最终上限已被证明,考虑到输入时间延迟.
- 排除了Zeno行为,验证了拟议的基于ESO的ET-SMC的可行性.
结论:
- 拟议的ET-SMC方法表现出卓越的稳定性,干扰减弱,跟踪精度和计算效率.
- 这种方法导致更稳定的恒星追踪器性能,增强精确的飞机导航.
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